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Record 1 2010-03-01

English

Subject field(s)
  • Aerodynamics and Theory of Gases
CONT

When a normal shock wave interacts with a boundary layer along a wall surface in supersonic internal flows and the shock is strong enough to separate the boundary layer, the shock is bifurcated and a series of shocks called "shock train" is formed.

French

Domaine(s)
  • Théorie des gaz et aérodynamique

Spanish

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